WO2022178118A1 - Method for enhancing bonding surface of difficult to bond plastics and laminate - Google Patents
Method for enhancing bonding surface of difficult to bond plastics and laminate Download PDFInfo
- Publication number
- WO2022178118A1 WO2022178118A1 PCT/US2022/016782 US2022016782W WO2022178118A1 WO 2022178118 A1 WO2022178118 A1 WO 2022178118A1 US 2022016782 W US2022016782 W US 2022016782W WO 2022178118 A1 WO2022178118 A1 WO 2022178118A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- adhesive
- laminate
- thermoplastic
- metal oxide
- adherent layer
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract description 17
- 239000004033 plastic Substances 0.000 title description 4
- 229920003023 plastic Polymers 0.000 title description 4
- 230000002708 enhancing effect Effects 0.000 title description 2
- 239000000853 adhesive Substances 0.000 claims abstract description 27
- 230000001070 adhesive effect Effects 0.000 claims abstract description 27
- 239000000758 substrate Substances 0.000 claims abstract description 25
- 229920001169 thermoplastic Polymers 0.000 claims abstract description 24
- 239000004416 thermosoftening plastic Substances 0.000 claims abstract description 24
- 229910044991 metal oxide Inorganic materials 0.000 claims abstract description 22
- 150000004706 metal oxides Chemical class 0.000 claims abstract description 22
- 230000001464 adherent effect Effects 0.000 claims abstract description 17
- 239000002243 precursor Substances 0.000 claims abstract description 14
- 239000000126 substance Substances 0.000 claims abstract description 8
- -1 nickel alkoxide Chemical class 0.000 claims description 13
- 239000000203 mixture Substances 0.000 claims description 10
- 229910019142 PO4 Inorganic materials 0.000 claims description 5
- 235000021317 phosphate Nutrition 0.000 claims description 5
- VVQNEPGJFQJSBK-UHFFFAOYSA-N Methyl methacrylate Chemical compound COC(=O)C(C)=C VVQNEPGJFQJSBK-UHFFFAOYSA-N 0.000 claims description 3
- BOTDANWDWHJENH-UHFFFAOYSA-N Tetraethyl orthosilicate Chemical compound CCO[Si](OCC)(OCC)OCC BOTDANWDWHJENH-UHFFFAOYSA-N 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 3
- 239000010452 phosphate Substances 0.000 claims description 3
- IBDVWXAVKPRHCU-UHFFFAOYSA-N 2-(2-methylprop-2-enoyloxy)ethyl 3-oxobutanoate Chemical compound CC(=O)CC(=O)OCCOC(=O)C(C)=C IBDVWXAVKPRHCU-UHFFFAOYSA-N 0.000 claims description 2
- SJIXRGNQPBQWMK-UHFFFAOYSA-N 2-(diethylamino)ethyl 2-methylprop-2-enoate Chemical compound CCN(CC)CCOC(=O)C(C)=C SJIXRGNQPBQWMK-UHFFFAOYSA-N 0.000 claims description 2
- VXEGSRKPIUDPQT-UHFFFAOYSA-N 4-[4-(4-methoxyphenyl)piperazin-1-yl]aniline Chemical compound C1=CC(OC)=CC=C1N1CCN(C=2C=CC(N)=CC=2)CC1 VXEGSRKPIUDPQT-UHFFFAOYSA-N 0.000 claims description 2
- IAYPIBMASNFSPL-UHFFFAOYSA-N Ethylene oxide Chemical compound C1CO1 IAYPIBMASNFSPL-UHFFFAOYSA-N 0.000 claims description 2
- 239000004696 Poly ether ether ketone Substances 0.000 claims description 2
- 239000004952 Polyamide Substances 0.000 claims description 2
- 239000004698 Polyethylene Substances 0.000 claims description 2
- 239000004734 Polyphenylene sulfide Substances 0.000 claims description 2
- 239000004743 Polypropylene Substances 0.000 claims description 2
- AHGFXGSMYLFWEC-UHFFFAOYSA-N [SiH4].CC(=C)C(O)=O Chemical compound [SiH4].CC(=C)C(O)=O AHGFXGSMYLFWEC-UHFFFAOYSA-N 0.000 claims description 2
- 150000001335 aliphatic alkanes Chemical class 0.000 claims description 2
- 150000001336 alkenes Chemical class 0.000 claims description 2
- QUZSUMLPWDHKCJ-UHFFFAOYSA-N bisphenol A dimethacrylate Chemical class C1=CC(OC(=O)C(=C)C)=CC=C1C(C)(C)C1=CC=C(OC(=O)C(C)=C)C=C1 QUZSUMLPWDHKCJ-UHFFFAOYSA-N 0.000 claims description 2
- 229920001400 block copolymer Polymers 0.000 claims description 2
- AGGUVAQPASULHN-UHFFFAOYSA-N butanedioic acid;2-hydroxyethyl 2-methylprop-2-enoate Chemical compound OC(=O)CCC(O)=O.CC(=C)C(=O)OCCO AGGUVAQPASULHN-UHFFFAOYSA-N 0.000 claims description 2
- 229920001577 copolymer Polymers 0.000 claims description 2
- UQEAIHBTYFGYIE-UHFFFAOYSA-N hexamethyldisiloxane Chemical group C[Si](C)(C)O[Si](C)(C)C UQEAIHBTYFGYIE-UHFFFAOYSA-N 0.000 claims description 2
- 150000003013 phosphoric acid derivatives Chemical class 0.000 claims description 2
- 229920002647 polyamide Polymers 0.000 claims description 2
- 229920002577 polybenzoxazole Polymers 0.000 claims description 2
- 229920000728 polyester Polymers 0.000 claims description 2
- 229920002530 polyetherether ketone Polymers 0.000 claims description 2
- 229920000573 polyethylene Polymers 0.000 claims description 2
- 229920000139 polyethylene terephthalate Polymers 0.000 claims description 2
- 239000005020 polyethylene terephthalate Substances 0.000 claims description 2
- 229920000642 polymer Polymers 0.000 claims description 2
- 229920000069 polyphenylene sulfide Polymers 0.000 claims description 2
- 229920001155 polypropylene Polymers 0.000 claims description 2
- 239000005049 silicon tetrachloride Substances 0.000 claims description 2
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 claims 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical group O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims 2
- 229910052814 silicon oxide Inorganic materials 0.000 claims 2
- 229910005855 NiOx Inorganic materials 0.000 claims 1
- 239000003522 acrylic cement Substances 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 abstract description 4
- 239000007789 gas Substances 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 238000000151 deposition Methods 0.000 description 4
- 230000008021 deposition Effects 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000004381 surface treatment Methods 0.000 description 4
- 238000011282 treatment Methods 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- BLRPTPMANUNPDV-UHFFFAOYSA-N Silane Chemical compound [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 description 2
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 2
- 230000004913 activation Effects 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005229 chemical vapour deposition Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 229910000077 silane Inorganic materials 0.000 description 2
- 150000003673 urethanes Chemical class 0.000 description 2
- 238000005169 Debye-Scherrer Methods 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 239000002318 adhesion promoter Substances 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000012298 atmosphere Substances 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 125000003178 carboxy group Chemical group [H]OC(*)=O 0.000 description 1
- 150000001768 cations Chemical class 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000001010 compromised effect Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 230000032798 delamination Effects 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 229910052733 gallium Inorganic materials 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 1
- 238000010849 ion bombardment Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 238000010297 mechanical methods and process Methods 0.000 description 1
- 150000002734 metacrylic acid derivatives Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000002086 nanomaterial Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 150000003014 phosphoric acid esters Chemical class 0.000 description 1
- 238000009832 plasma treatment Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
- B29C65/485—Multi-component adhesives, i.e. chemically curing as a result of the mixing of said multi-components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
- B29C66/026—Chemical pre-treatments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/45—Joining of substantially the whole surface of the articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3055—Cars
Definitions
- the present invention in general relates to surface treatments, and in particular to a plastic surface treatment amenable to adhesive bonding.
- a method of bonding includes providing a thermoplastic substrate having a surface with a surface energy value of less than a 48 miliJoules per meter squared. The surface is exposed to particulate formed in a combustion flame from a precursor. The particulate forms an adherent layer of metal oxide on the surface. An adhesive is applied to the adherent layer. A second substance is placed in in simultaneous contact with the adhesive to bond the thermoplastic.
- a laminate includes a thermoplastic substrate having a surface with a surface energy value of less than a 48 miliJoules per meter squared.
- An adherent layer of metal oxide is on a surface of the thermoplastic substrate.
- An adhesive is attached to the adherent layer.
- a second substance is in simultaneous contact with the adhesive.
- FIG. 1 is a schematic of an inventive method for formation of adherent layer of metal oxide on a surface of the substrate; and [0011] FIG.2 is a cross sectional view of an inventive laminate.
- the present invention has utility as a method of forming a layer of metal oxide on low surface energy thermoplastic target substrate. Unlike conventional techniques that apply such layers under reduced pressure, using complex plasma, or under conditions that can deform or otherwise damage a thermoplastic substrate molded into a complex shape; the present invention efficiently applies an adherent layer of metal oxide on the thermoplastic surface to which an adhesive is directly applied. A second substance placed in in simultaneous contact with the adhesive is bonded to the thermoplastic.
- thermoplastic substrates are used in general industrial and transportation markets, where the use of such plastics for strength and light-weighting is desired.
- the present invention allows for common metals, coated metal clips, or vehicle structure to be structurally bonded to the thermoplastic or to manufacture a given article from the thermoplastic.
- the present invention minimizes or eliminates the use of mechanical fasteners, vibration welding or other long processes or chemical treatment processes thereby reducing scrappage and manufacturing time.
- metal oxide is defined as a MO x where M is a cation of Ni, Si, B, Co, Fe, Cu, Al, Ga, or Sn, and x is an rational number of between 0.8-1.0 for +2 M oxidation states and 1.4 and 2.0 for +4M oxidation states.
- the metal oxide being amorphous or having crystalline domain sizes of from 1 to 200 nm as measured by Debye-Scherrer line broadening.
- the present invention modifies a thermoplastic as a substrate having a surface energy value of less than a 48 miliJoules per meter squared.
- Thermoplastic substrates operative herein illustratively include polyethylene, polypropylene, polyethylene terephthalate, disparpolypropylenes, polyamides, polyesters, polyether ether ketones, polybenzobisoxazoles, polyphenylene sulfide, and block copolymers containing at least of one of the aforementioned constituting at least 40 percent by weight of the copolymer; and blends thereof.
- the present invention affords a layer of metal oxide that is deposited by combustion chemical vapor deposition (C-CVD). A uniform flame nozzle is extendible over a linear extent of from 0.01 to 6 meters, or even more so as produce a layer of metal oxide with a controlled rate of deposition across the linear extent.
- a schematic of an inventive system applying a layer of metal oxide is shown in general at 10.
- the system includes an inlet 12 for a combustible gas.
- a combustible gas operative herein illustratively includes a C 1 -C 6 alkane, a C 2 -C 6 alkene, ethylene oxide, and combinations thereof.
- a metal containing precursor inlet 14 is also delivered to gas burner 16.
- an air or oxygen inlet 15 is also provided.
- the ratio of the combustible gas: metal containing precursor is readily adjusted to control the stoichiometry of metal:oxygen.
- a flame 18 is generated in which particles 20 of metal oxide and precursors thereof are formed.
- Parameters that control the composition and deposition rate includes: combustible flow rate, air flow rate, precursor flow rate, precursor concentration, distance between surface and burner tip, and translation rate of substrate stage.
- Typical operation conditions according to the present invention include Typical process conditions for layer formation include a burner air flow of 0.1 to 100 SLM, an air-to-combustible ratio of 1000:1 to 2:1, a burner tip to surface distance of between 1 and 300 mm, and a stage linear velocity of about 50 mm/sec, and a flame length of from 1 to 50 mm from the surface 26 of the substrate 22 to be coated.
- the particulate 20 condenses to form a layer of metal oxide 22 adherent to a surface 25 of a substrate 24. While the surface 25 is depicted as planar, it is appreciated that the surface is also readily formed as in the shape of a planar curve, a complex three dimensional shape, or a combination thereof.
- a substrate stage 26 is depicted as translating from right to left to deposit a layer 22. It is appreciated that the stage 26 can move in various directions including vertical relative to the burner tip 17. In still other embodiments, the burner 16 is movable. In still other embodiments, the stage 26 includes a heating element or a cooling element to control the temperature of the substrate 24.
- a typical thickness of a layer 22 is between 5 and 5000 nanometers (nm) and typical deposition to these thicknesses range from 5 to 300 seconds.
- Precursors operative herein illustratively include hexamethyldisiloxane.
- the precursor is volatile while in other instances, a solution of the precursor can be atomized/nebulized sufficiently, the atomized solution functions as gas and can be transferred to the flame without requiring an appreciable vapor pressure from the precursor.
- the metal oxide layer has surface polar moieties of hydroxyl, carboxyl, and ylides, and lone pairs capable of forming covalent dative bonds. The surface polar moieties are amenable to reaction with an adhesive applied thereon.
- adhesive 32 is applied onto the layer of metal oxide 22.
- Adhesives operative herein illustratively include two or one part urethanes, two-part methyl methacrylate, acrylic adhesives, mixtures thereof, and hybrids thereof.
- the adhesive 32 contains silane adhesion promotors or silane functional elements.
- Adhesion promoters operative herein illustratively include phosphate esters; phosphate ester polymers; mixtures of mono- and di-functional phosphates; functionalized methacrylates such as hydroxyethylmethacrylate succinate, acetoacetoxy ethyl methacrylate, N,N-diethylaminoethyl methacrylate, ethoxylated bisphenol A dimethacrylate and methacrylate silanes and combinations thereof.
- a silanizing agent modifies the substrate surface to achieve improved surface bonding of inventive composition compared to formulations lacking the same by modifying the hydrophobicity of the substrate surface.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Laminated Bodies (AREA)
Abstract
A method of bonding includes providing a thermoplastic substrate having a surface with a surface energy value of less than a 48 miliJoules per meter squared. The surface is exposed to particulate formed in a combustion flame from a precursor. The particulate forms an adherent layer of metal oxide on the surface. An adhesive is applied to the adherent layer. A second substance is placed in in simultaneous contact with the adhesive to bond the thermoplastic. A laminate is provided that includes a thermoplastic substrate having a surface. An adherent layer of metal oxide is on a surface of the thermoplastic substrate. An adhesive is attached to the adherent layer. A second substance is in simultaneous contact with the adhesive.
Description
METHOD FOR ENHANCING BONDING SURFACE OF DIFFICULT TO BOND
PLASTICS AND LAMINATE
RELATED APPLICATIONS
[0001] This application claims priority benefit of US Application Serial Number 17/673,129 filed February 16, 2022 that in turn claim priority benefit of US Provisional Application Serial Number 63/150,740 filed February 18, 2021; the contents of which are hereby incorporated by reference.
FIELD OF THE INVENTION
[0002] The present invention in general relates to surface treatments, and in particular to a plastic surface treatment amenable to adhesive bonding.
BACKGROUND OF THE INVENTION
[0003] The ability to adhesively bond to a surface with a limited number of available bonding sites and characterized by a surface energy value of less than approximately 48 miliJoules per meter squared (mJ/m2) has been addressed in the past through surface activation of the low energy surface through various treatments such as exposure to flame, plasma, ion bombardment, or other processes to create reactive moieties to which an adhesive could bond. While such low energy surface modification treatments proved effective, they have met with limited acceptance owing to the cost, limited duration of surface activation, and the impracticality of surface treatment in field usage or to bond large area substrates. [0004] Resort to primer compositions intermediate between a low energy surface and an adhesive were found to address in part the limitations of high energy surface treatments, yet such primers add to the cost and complexity of bonding thereby limiting instances of practical
usage. Additionally, the strength of low energy surfaces adhesively bonded through resort to primers has compromised strength owing to interfacial delamination. [0005] Despite the numerous advantages of structural adhesives over the more traditional mechanical methods of joining, such as by clamps, nuts and bolts, etc., one of the most important reasons these aforementioned adhesives have not made more sizable inroads into industrial bonding applications. [0006] Thus, there exists a need for an enhanced low surface energy bonding treatment to traditional adhesives such as two or one part urethanes, two part methyl methacrylate, and acrylic adhesives and without resort to conventional adhesion promotors or aggressive plasma treatments. SUMMARY OF THE INVENTION [0007] A method of bonding includes providing a thermoplastic substrate having a surface with a surface energy value of less than a 48 miliJoules per meter squared. The surface is exposed to particulate formed in a combustion flame from a precursor. The particulate forms an adherent layer of metal oxide on the surface. An adhesive is applied to the adherent layer. A second substance is placed in in simultaneous contact with the adhesive to bond the thermoplastic. [0008] A laminate is provided that includes a thermoplastic substrate having a surface with a surface energy value of less than a 48 miliJoules per meter squared. An adherent layer of metal oxide is on a surface of the thermoplastic substrate. An adhesive is attached to the adherent layer. A second substance is in simultaneous contact with the adhesive.
BRIEF DESCRIPTION OF THE DRAWINGS [0009] The present invention is further detailed with respect to the following drawings that are intended to show certain aspects of the present invention but should not be construed as a limit on the practice of the present invention. The relative dimensions of layers are distorted with visual clarity. [0010] FIG. 1 is a schematic of an inventive method for formation of adherent layer of metal oxide on a surface of the substrate; and [0011] FIG.2 is a cross sectional view of an inventive laminate. DETAILED DESCRIPTION OF THE INVENTION [0012] The present invention has utility as a method of forming a layer of metal oxide on low surface energy thermoplastic target substrate. Unlike conventional techniques that apply such layers under reduced pressure, using complex plasma, or under conditions that can deform or otherwise damage a thermoplastic substrate molded into a complex shape; the present invention efficiently applies an adherent layer of metal oxide on the thermoplastic surface to which an adhesive is directly applied. A second substance placed in in simultaneous contact with the adhesive is bonded to the thermoplastic. [0013] Typical thermoplastic substrates are used in general industrial and transportation markets, where the use of such plastics for strength and light-weighting is desired. In particular here, the present invention allows for common metals, coated metal clips, or vehicle structure to be structurally bonded to the thermoplastic or to manufacture a given article from the thermoplastic. As a result, the present invention minimizes or eliminates the use of mechanical fasteners, vibration welding or other long processes or chemical treatment processes thereby reducing scrappage and manufacturing time.
[0014] The present invention will now be described with reference to the following embodiments. As is apparent by these descriptions, this invention can be embodied in different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art. For example, features illustrated with respect to one embodiment can be incorporated into other embodiments, and features illustrated with respect to a particular embodiment may be deleted from the embodiment. In addition, numerous variations and additions to the embodiments suggested herein will be apparent to those skilled in the art in light of the instant disclosure, which do not depart from the instant invention. Hence, the following specification is intended to illustrate some particular embodiments of the invention, and not to exhaustively specify all permutations, combinations, and variations thereof. [0015] It is to be understood that in instances where a range of values are provided that the range is intended to encompass not only the end point values of the range but also intermediate values of the range as explicitly being included within the range and varying by the last significant figure of the range. By way of example, a recited range of from 1 to 4 is intended to include 1-2, 1-3, 2-4, 3-4, and 1-4. [0016] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. [0017] Unless indicated otherwise, explicitly or by context, the following terms are used herein as set forth below. As used in the description of the invention and the appended claims, the singular forms “a,” “an” and “the” are intended to include the plural forms as
well, unless the context clearly indicates otherwise. Also as used herein, “and/or” refers to and encompasses any and all possible combinations of one or more of the associated listed items, as well as the lack of combinations when interpreted in the alternative (“or”). [0018] As used herein, metal oxide is defined as a MOx where M is a cation of Ni, Si, B, Co, Fe, Cu, Al, Ga, or Sn, and x is an rational number of between 0.8-1.0 for +2 M oxidation states and 1.4 and 2.0 for +4M oxidation states. The metal oxide being amorphous or having crystalline domain sizes of from 1 to 200 nm as measured by Debye-Scherrer line broadening. [0019] The present invention modifies a thermoplastic as a substrate having a surface energy value of less than a 48 miliJoules per meter squared. Thermoplastic substrates operative herein illustratively include polyethylene, polypropylene, polyethylene terephthalate, disparpolypropylenes, polyamides, polyesters, polyether ether ketones, polybenzobisoxazoles, polyphenylene sulfide, and block copolymers containing at least of one of the aforementioned constituting at least 40 percent by weight of the copolymer; and blends thereof. [0020] The present invention affords a layer of metal oxide that is deposited by combustion chemical vapor deposition (C-CVD). A uniform flame nozzle is extendible over a linear extent of from 0.01 to 6 meters, or even more so as produce a layer of metal oxide with a controlled rate of deposition across the linear extent. The deposition is controlled to provide a uniformity of thickness across the linear extent or has varied combustions zones to create areas that are of greater or lesser thickness in a given region. The present invention applies a layer of metal oxide while the thermoplastic substrate is maintained at atmosphere pressure. [0021] A schematic of an inventive system applying a layer of metal oxide is shown in general at 10. The system includes an inlet 12 for a combustible gas. A combustible gas
operative herein illustratively includes a C1-C6 alkane, a C2-C6 alkene, ethylene oxide, and combinations thereof. A metal containing precursor inlet 14 is also delivered to gas burner 16. In some embodiments, an air or oxygen inlet 15 is also provided. The ratio of the combustible gas: metal containing precursor is readily adjusted to control the stoichiometry of metal:oxygen. Upon ignition of the gas mixture from the burner tip 17, a flame 18 is generated in which particles 20 of metal oxide and precursors thereof are formed. Parameters that control the composition and deposition rate includes: combustible flow rate, air flow rate, precursor flow rate, precursor concentration, distance between surface and burner tip, and translation rate of substrate stage. Typical operation conditions according to the present invention include Typical process conditions for layer formation include a burner air flow of 0.1 to 100 SLM, an air-to-combustible ratio of 1000:1 to 2:1, a burner tip to surface distance of between 1 and 300 mm, and a stage linear velocity of about 50 mm/sec, and a flame length of from 1 to 50 mm from the surface 26 of the substrate 22 to be coated. [0022] The particulate 20 condenses to form a layer of metal oxide 22 adherent to a surface 25 of a substrate 24. While the surface 25 is depicted as planar, it is appreciated that the surface is also readily formed as in the shape of a planar curve, a complex three dimensional shape, or a combination thereof. A substrate stage 26 is depicted as translating from right to left to deposit a layer 22. It is appreciated that the stage 26 can move in various directions including vertical relative to the burner tip 17. In still other embodiments, the burner 16 is movable. In still other embodiments, the stage 26 includes a heating element or a cooling element to control the temperature of the substrate 24. [0023] A typical thickness of a layer 22 is between 5 and 5000 nanometers (nm) and typical deposition to these thicknesses range from 5 to 300 seconds. [0024] Precursors operative herein illustratively include hexamethyldisiloxane. tetraethoxysilane, tetraethylorthosilicate, silicon tetrachloride, nickel alkoxides, and
combinations thereof. In some inventive embodiments, the precursor is volatile while in other instances, a solution of the precursor can be atomized/nebulized sufficiently, the atomized solution functions as gas and can be transferred to the flame without requiring an appreciable vapor pressure from the precursor. [0025] Without intending to be bound to a particular theory, it is believed that the metal oxide layer has surface polar moieties of hydroxyl, carboxyl, and ylides, and lone pairs capable of forming covalent dative bonds. The surface polar moieties are amenable to reaction with an adhesive applied thereon. The nanostructure of the layer of metal oxide with an increased surface area relative the surface of the substrate also enhances bonding. [0026] As shown in FIG. 2, adhesive 32 is applied onto the layer of metal oxide 22. Adhesives operative herein illustratively include two or one part urethanes, two-part methyl methacrylate, acrylic adhesives, mixtures thereof, and hybrids thereof. In some inventive embodiments, the adhesive 32 contains silane adhesion promotors or silane functional elements. Adhesion promoters operative herein illustratively include phosphate esters; phosphate ester polymers; mixtures of mono- and di-functional phosphates; functionalized methacrylates such as hydroxyethylmethacrylate succinate, acetoacetoxy ethyl methacrylate, N,N-diethylaminoethyl methacrylate, ethoxylated bisphenol A dimethacrylate and methacrylate silanes and combinations thereof. In still other embodiments, a silanizing agent modifies the substrate surface to achieve improved surface bonding of inventive composition compared to formulations lacking the same by modifying the hydrophobicity of the substrate surface. [0027] The present invention is further detailed with respect to the following examples. These examples are illustrative of specific embodiments of the present invention and not intended to limit the scope of the appended claims.
[0028] As a person skilled in the art will recognize from the previous detailed description and from the figures and claims, modifications and changes can be made to the preferred embodiments of the invention without departing from the scope of this invention defined in the following claims.
Claims
CLAIMS 1. A method of bonding a thermoplastic comprising: providing a thermoplastic substrate having a surface with a surface energy value of less than a 48 miliJoules per meter squared; exposing the surface to particulate formed in a flame from a precursor; forming the particulate into an adherent layer of metal oxide on the surface; applying an adhesive to the adherent layer; and attaching a second substance in in simultaneous contact with said adhesive to bond the thermoplastic. 2. The method of claim 1, wherein the layer is SiOx. 3. The method of claim 2, wherein the precursor is hexamethyldisiloxane, tetraethylorthosilicate, or silicon tetrachloride. 5. The method of claim 1, wherein the layer is NiOx. 6. The method of claim 5, wherein the precursor is a nickel alkoxide. 7. The method of any one of claims 1 to 6, wherein said adherent layer of metal oxide is substantially uniform. 8. The method of any one of claims 1 to 7, further comprising a combustible gas that is optionally one or more of a C1-C6 alkane, a C2-C6 alkene, ethylene oxide, or a combination thereof. 9. A laminate formed according to any one of claims 1 to 8 comprising: a thermoplastic substrate: an adherent layer of metal oxide on a surface of the thermoplastic substrate;
an adhesive to the adherent layer; and a second substance in in simultaneous contact with said adhesive. 10. The laminate of claim 9, wherein said thermoplastic is one of: polyethylene, polypropylene, polyethylene terephthalate, disparpolypropylenes, polyamides, polyesters, polyether ether ketones, polybenzobisoxazoles, polyphenylene sulfide, or block copolymers containing at least of one of the aforementioned constituting at least 40 percent by weight of the copolymer; orblends thereof. 11. The laminate of claim 9, wherein said adherent layer of metal oxide is from 5 to 5000 nm in thickness. 12. The laminate of claim 9, wherein the layer is SiOx. 13. The laminate of claim 9, wherein said adhesive is at least one of: a two part urethane, a one part urethane, a two-part methyl methacrylate, an acrylic adhesive, mixtures thereof, and hybrids thereof. 14. The laminate of claim 9, wherein said adhesive further comprises an adhesion promotor that is optionally one or more a phosphate ester, a phosphate ester polymer; a mixture of mono- and di-functional phosphates, a hydroxyethylmethacrylate succinate, an acetoacetoxy ethyl methacrylate, N,N-diethylaminoethyl methacrylate, ethoxylated bisphenol A dimethacrylate, a methacrylate silane, or a combination thereof. 15. An automotive part formed from the laminate of any one of claims 9 to 14.
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US202163150740P | 2021-02-18 | 2021-02-18 | |
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US17/673,129 US20220259459A1 (en) | 2021-02-18 | 2022-02-16 | Method for enhancing bonding surface of difficult to bond plastics |
US17/673,129 | 2022-02-16 |
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Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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WO2012140873A1 (en) * | 2011-04-15 | 2012-10-18 | 株式会社日立製作所 | Method for laser bonding |
DE102014214751A1 (en) * | 2014-07-28 | 2016-01-28 | Leibniz-Institut Für Polymerforschung Dresden E.V. | MODIFIED PLASTIC SURFACES AND METHOD FOR THEIR PRODUCTION |
WO2019240063A1 (en) * | 2018-06-14 | 2019-12-19 | 横浜ゴム株式会社 | Method for manufacturing laminate member |
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Publication number | Priority date | Publication date | Assignee | Title |
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WO2012140873A1 (en) * | 2011-04-15 | 2012-10-18 | 株式会社日立製作所 | Method for laser bonding |
DE102014214751A1 (en) * | 2014-07-28 | 2016-01-28 | Leibniz-Institut Für Polymerforschung Dresden E.V. | MODIFIED PLASTIC SURFACES AND METHOD FOR THEIR PRODUCTION |
WO2019240063A1 (en) * | 2018-06-14 | 2019-12-19 | 横浜ゴム株式会社 | Method for manufacturing laminate member |
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